Patent · US Active

Aircraft power electronic unit and method of cooling

US11134585B2 · kind B2 · utility

2Cited by
4References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 31, 2019
Grant dateSep 28, 2021
Priority date
Expiry dateMay 31, 2039

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D41/00
  • WIPO fieldAudio-visual technology
  • WIPO sectorElectrical engineering

Abstract

An electrical power unit cooling system including at least one cooling fin configured to be thermally connected to a bus housing of the electrical power unit, the bus housing being configured to be attached to a surface of an aircraft fan housing such that the at least one cooling fin protrudes through the fan housing in order to be cooled by air flow within the fan housing.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.